[Isocops] IBEX Orbit# 184 ATS (24 Nov 12 - 2 Nov 12)
Ibex Mission Operations
ibexops at gmail.com
Thu Oct 11 13:51:25 EDT 2012
Guys,
Here are the planning and ATS files for Orbit# 184.
Orbit# 184 will also include the LUT Upload.
The ATS files have not been placed on the SFTP server so that Ken can check
them individually.
1*.IBEX_2012_298_o0184a_postverif_asc_v001.scr* was generated with
Ascending payload commands only within the STF
==========================
SOFT CONSTRAINT VIOLATIONS
==========================
IBX-CLC-003: Payload mode is HVSCI during interval 2012/10/28 22:24:19 UTC -
2012/10/28 22:34:19 UTC, which overlaps 5N thruster maneuver at
2012/10/28 22:24:19 UTC - 2012/10/28 22:34:19 UTC
IBX-CLC-008: Spacecraft state is HK during interval 2012/10/26 03:45:00 UTC
-
2012/10/26 03:59:30 UTC, which overlaps HVSCI payload mode at
2012/10/26 03:45:00 UTC - 2012/10/26 03:59:30 UTC
IBX-CLC-008: Spacecraft state is HK during interval 2012/10/26 03:59:30 UTC
-
2012/10/29 18:25:00 UTC, which overlaps HVSCI payload mode at
2012/10/26 03:59:30 UTC - 2012/10/29 18:25:00 UTC
--
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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; Filename: IBEX_2012_298_o0184a_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/285.164914
; Plan period start: 2012/299.031900
; Plan period stop: 2012/308.002200
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_298_o0184a_v001.oef
; IBEX_2012_298_o0184a_v002.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_25_03_19_00()
begin
# Orbit# 184 Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/10:25:03:22:33
@FCT_SetScState science $TIME=2012/10:25:03:22:35
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/10:25:03:22:37
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/10:25:03:22:39
# Orbit# 184 Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:25:10:00:21
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:25:10:00:37
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/10:25:10:11:31
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:25:10:11:34
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/10:25:10:11:38
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/10:25:10:11:42
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/10:25:10:11:59
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:25:10:12:02
# Orbit# 184 APOGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:28:20:39:30
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/10:28:20:40:12
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/10:28:20:50:31
# Orbit# 184 APOGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/10:28:21:24:21
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:28:21:29:19
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:28:22:14:19
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:28:22:14:20
@FCT_SetFcMode burn $TIME=2012/10:28:22:21:19
@ACT_SetInrDir -0.832247,-0.50355,-0.231952 $TIME=2012/10:28:22:22:19
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:28:22:23:19
@ACT_SetThrustTime 660 $TIME=2012/10:28:22:24:14
@ACT_SetThrustEnable ENABLE $TIME=2012/10:28:22:24:19
@ACT_SetThrustEnable DISABLE $TIME=2012/10:28:22:34:19
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:28:22:34:20
@ACT_SetThrustTime 0 $TIME=2012/10:28:22:34:49
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:28:22:49:29
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:28:22:49:39
@FCT_SetFcMode Mission $TIME=2012/10:28:22:50:19
# Orbit# 184 APOGEE: Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/10:28:23:39:25
@FCT_SetScState science $TIME=2012/10:28:23:39:27
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/10:28:23:39:29
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/10:28:23:39:31
# Orbit# 184 APOGEE: Ascending IBEX_Hi Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:29:00:09:25
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:29:00:09:41
@CEU_SET_PARAMETER 1, TLM_RATE_SOH $TIME=2012/10:29:00:20:35
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:29:00:20:38
@CEU_SET_PARAMETER 3, HV_STEP_FRAC $TIME=2012/10:29:00:20:42
@CEU_HI_CEM_4_LVL 1800 $TIME=2012/10:29:00:20:46
@CEU_SET_PARAMETER 0, TLM_RATE_SOH $TIME=2012/10:29:00:21:03
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:29:00:21:06
# Orbit# 184 PERIGEE: Descending IBEX_Hi Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:02:07:16:06
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:02:07:16:48
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:02:07:27:07
# Orbit# 184 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:02:13:57:50
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:02:14:00:40
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:02:14:45:40
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:02:14:45:41
@FCT_SetFcMode burn $TIME=2012/11:02:14:52:40
@ACT_SetInrDir -0.786493,-0.561456,-0.257285 $TIME=2012/11:02:14:53:40
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:02:14:54:40
@ACT_SetThrustTime 660 $TIME=2012/11:02:14:55:35
@ACT_SetThrustEnable ENABLE $TIME=2012/11:02:14:55:40
@ACT_SetThrustEnable DISABLE $TIME=2012/11:02:15:05:40
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:02:15:05:41
@ACT_SetThrustTime 0 $TIME=2012/11:02:15:06:10
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:02:15:20:50
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:02:15:21:00
@FCT_SetFcMode Mission $TIME=2012/11:02:15:21:40
end
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; Filename: IBEX_2012_298_o0184a_Lo_Commands_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/285.163724
; Plan period start: 2012/299.031900
; Plan period stop: 2012/308.002200
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_298_o0184a_v001.oef
; IBEX_2012_298_o0184a_Lo_Commands_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_25_03_19_00()
begin
# Orbit# 184 Ascending IBEX_Lo Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:25:10:14:07
@CEU_SET_PARAMETER 1, TLM_RATE_SOH_LO $TIME=2012/10:25:10:14:23
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:25:10:14:32
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/10:25:10:14:34
@CEU_LO_PMT_LVL 800 $TIME=2012/10:25:10:14:35
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:25:10:14:58
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/10:25:10:15:14
@CEU_LO_COL_NEG_LVL 400 $TIME=2012/10:25:10:15:16
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:25:10:16:37
@CEU_LO_IF_PAC_VSET 7000 $TIME=2012/10:25:10:16:39
@CEU_LO_IF_MCP_VSET 2854 $TIME=2012/10:25:10:19:31
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/10:25:10:21:51
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/10:25:10:21:53
@CEU_LO_U_POS_LVL 0 $TIME=2012/10:25:10:21:55
@CEU_LO_U_NEG_LVL 0 $TIME=2012/10:25:10:22:09
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:25:10:22:25
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:25:10:22:27
@CEU_SET_PARAMETER 0, TLM_RATE_SOH_LO $TIME=2012/10:25:10:22:28
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:25:10:22:45
# Orbit# 184 APOGEE: Descending IBEX_Lo Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:28:20:28:21
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:28:20:29:05
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/10:28:20:29:07
@CEU_LO_PMT_LVL 640 $TIME=2012/10:28:20:29:10
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:28:20:29:33
@CEU_LO_IF_PAC_VSET 5500 $TIME=2012/10:28:20:29:35
@CEU_LO_IF_MCP_VSET 2083 $TIME=2012/10:28:20:32:27
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/10:28:20:35:11
@CEU_LO_COL_NEG_LVL 216 $TIME=2012/10:28:20:35:13
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/10:28:20:36:29
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/10:28:20:36:31
@CEU_LO_U_POS_LVL 0 $TIME=2012/10:28:20:36:32
@CEU_LO_U_NEG_LVL 0 $TIME=2012/10:28:20:36:46
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:28:20:37:01
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:28:20:37:03
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:28:20:37:25
# Orbit# 184 APOGEE: Inertial Maneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:28:21:29:19
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:28:22:14:19
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:28:22:14:20
# @FCT_SetFcMode burn $TIME=2012/10:28:22:21:19
# @ACT_SetInrDir -0.832247,-0.50355,-0.231952 $TIME=2012/10:28:22:22:19
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:28:22:23:19
# @ACT_SetThrustTime 660 $TIME=2012/10:28:22:24:14
# @ACT_SetThrustEnable ENABLE $TIME=2012/10:28:22:24:19
# @ACT_SetThrustEnable DISABLE $TIME=2012/10:28:22:34:19
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:28:22:34:20
# @ACT_SetThrustTime 0 $TIME=2012/10:28:22:34:49
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:28:22:49:29
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:28:22:49:39
# @FCT_SetFcMode Mission $TIME=2012/10:28:22:50:19
# Orbit# 184 APOGEE: Ascending IBEX_Lo Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:29:00:23:11
@CEU_SET_PARAMETER 1, TLM_RATE_SOH_LO $TIME=2012/10:29:00:23:27
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:29:00:23:36
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/10:29:00:23:38
@CEU_LO_PMT_LVL 800 $TIME=2012/10:29:00:23:39
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:29:00:24:02
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/10:29:00:24:18
@CEU_LO_COL_NEG_LVL 400 $TIME=2012/10:29:00:24:20
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:29:00:25:41
@CEU_LO_IF_PAC_VSET 7000 $TIME=2012/10:29:00:25:43
@CEU_LO_IF_MCP_VSET 2854 $TIME=2012/10:29:00:28:35
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/10:29:00:30:55
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/10:29:00:30:57
@CEU_LO_U_POS_LVL 0 $TIME=2012/10:29:00:30:59
@CEU_LO_U_NEG_LVL 0 $TIME=2012/10:29:00:31:13
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/10:29:00:31:29
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/10:29:00:31:31
@CEU_SET_PARAMETER 0, TLM_RATE_SOH_LO $TIME=2012/10:29:00:31:32
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:29:00:31:49
# Orbit# 184 PERIGEE: Descending IBEX_Lo Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:02:07:04:57
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:02:07:05:41
@CEU_SET_PARAMETER 16, HV_STEP_FRAC $TIME=2012/11:02:07:05:43
@CEU_LO_PMT_LVL 640 $TIME=2012/11:02:07:05:46
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:02:07:06:09
@CEU_LO_IF_PAC_VSET 5500 $TIME=2012/11:02:07:06:11
@CEU_LO_IF_MCP_VSET 2083 $TIME=2012/11:02:07:09:03
@CEU_SET_PARAMETER 11, HV_STEP_FRAC $TIME=2012/11:02:07:11:47
@CEU_LO_COL_NEG_LVL 216 $TIME=2012/11:02:07:11:49
@CEU_SET_PARAMETER 0, HV_STEP_DWELL $TIME=2012/11:02:07:13:05
@CEU_SET_PARAMETER 255, HV_STEP_FRAC $TIME=2012/11:02:07:13:07
@CEU_LO_U_POS_LVL 0 $TIME=2012/11:02:07:13:08
@CEU_LO_U_NEG_LVL 0 $TIME=2012/11:02:07:13:22
@CEU_SET_PARAMETER 4, HV_STEP_DWELL $TIME=2012/11:02:07:13:37
@CEU_SET_PARAMETER 1, HV_STEP_FRAC $TIME=2012/11:02:07:13:39
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:02:07:14:01
# Orbit# 184 PERIGEE: Inertial Maneuver Commands
# @ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:02:14:00:40
# @ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:02:14:45:40
# @ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:02:14:45:41
# @FCT_SetFcMode burn $TIME=2012/11:02:14:52:40
# @ACT_SetInrDir -0.786493,-0.561456,-0.257285 $TIME=2012/11:02:14:53:40
# @ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:02:14:54:40
# @ACT_SetThrustTime 660 $TIME=2012/11:02:14:55:35
# @ACT_SetThrustEnable ENABLE $TIME=2012/11:02:14:55:40
# @ACT_SetThrustEnable DISABLE $TIME=2012/11:02:15:05:40
# @ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:02:15:05:41
# @ACT_SetThrustTime 0 $TIME=2012/11:02:15:06:10
# @ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:02:15:20:50
# @ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:02:15:21:00
# @FCT_SetFcMode Mission $TIME=2012/11:02:15:21:40
end
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; Filename: IBEX_2012_298_o0184a_postverif_asc_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/285.163319
; Plan period start: 2012/299.031900
; Plan period stop: 2012/303.182500
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_298_o0184a_v001.oef
; IBEX_2012_298_o0184a_postverif_asc_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_25_03_19_00()
begin
# Orbit# 184 Ascending Payload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:26:03:45:00
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:26:03:45:30
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:26:03:57:00
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:26:03:59:30
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2012/10:26:04:00:00
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:26:04:08:30
# Orbit# 184 APOGEE: Inertial MAneuver
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:28:21:29:19
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:28:22:14:19
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:28:22:14:20
@FCT_SetFcMode burn $TIME=2012/10:28:22:21:19
@ACT_SetInrDir -0.832247,-0.50355,-0.231952 $TIME=2012/10:28:22:22:19
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:28:22:23:19
@ACT_SetThrustTime 660 $TIME=2012/10:28:22:24:14
@ACT_SetThrustEnable ENABLE $TIME=2012/10:28:22:24:19
@ACT_SetThrustEnable DISABLE $TIME=2012/10:28:22:34:19
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:28:22:34:20
@ACT_SetThrustTime 0 $TIME=2012/10:28:22:34:49
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:28:22:49:29
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:28:22:49:39
@FCT_SetFcMode Mission $TIME=2012/10:28:22:50:19
end
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; Filename: IBEX_2012_298_o0184a_desc_apo_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/285.150505
; Plan period start: 2012/299.032100
; Plan period stop: 2012/303.182500
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_298_o0184a_v001.oef
; IBEX_2012_298_o0184a_desc_apo_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_25_03_21_00()
begin
# Orbit# 184 APOGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:28:20:28:21
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2012/10:28:20:29:03
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:28:20:37:25
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/10:28:20:39:30
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/10:28:20:40:12
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/10:28:20:51:11
# Orbit# 184 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/10:28:21:24:21
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/10:28:21:29:19
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/10:28:22:14:19
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/10:28:22:14:20
@FCT_SetFcMode burn $TIME=2012/10:28:22:21:19
@ACT_SetInrDir -0.832247,-0.50355,-0.231952 $TIME=2012/10:28:22:22:19
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/10:28:22:23:19
@ACT_SetThrustTime 660 $TIME=2012/10:28:22:24:14
@ACT_SetThrustEnable ENABLE $TIME=2012/10:28:22:24:19
@ACT_SetThrustEnable DISABLE $TIME=2012/10:28:22:34:19
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/10:28:22:34:20
@ACT_SetThrustTime 0 $TIME=2012/10:28:22:34:49
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/10:28:22:49:29
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/10:28:22:49:39
@FCT_SetFcMode Mission $TIME=2012/10:28:22:50:19
end
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; Filename: IBEX_2012_298_o0184b_v001.scr
; File type: MAESTRO Absolute Time Sequence Script (ATS)
;
; Create time: 2012/285.145218
; Plan period start: 2012/303.182300
; Plan period stop: 2012/308.002400
; Default time format: UTC
;
; Input files: 2
; IBEX_2012_298_o0184a_v001.oef
; IBEX_2012_298_o0184a_arcb_v001.stf
; ATS_CMD_TIME_OFFSET = 0
script ats_2012_10_29_18_23_00()
begin
# Orbit# 184 APOGEE: ARC-B Ascending BUS Commands
@ACT_SetSpinPulseProtectEnable Disable $TIME=2012/10:28:23:39:25
@FCT_SetScState science $TIME=2012/10:28:23:39:27
@ACT_SetSpinPulseProtectEnable Enable $TIME=2012/10:28:23:39:29
@CEU_LO_SCIENCE_MODE NORMAL $TIME=2012/10:28:23:39:31
# Orbit# 184 APOGEE: ARC-B Ascending Payload Commands
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:29:00:09:25
@CEU_MACRO_EXEC ASCENDING_HI $TIME=2012/10:29:00:09:41
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:29:00:20:43
@CEU_MACRO_EXEC ASCENDING_PL1 $TIME=2012/10:29:00:22:48
@CEU_MACRO_EXEC ASCENDING_LO $TIME=2012/10:29:00:23:04
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/10:29:00:31:24
# Orbit# 184 PERIGEE: Descending Payload Commands
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:02:07:04:57
@CEU_MACRO_EXEC DESCENDING_LO $TIME=2012/11:02:07:05:39
@CEU_MACRO_EXEC ASCENDING_PL2 $TIME=2012/11:02:07:14:01
@CEU_MACRO_EXEC DESCENDING_PL1 $TIME=2012/11:02:07:16:06
@CEU_MACRO_EXEC DESCENDING_HI $TIME=2012/11:02:07:16:48
@CEU_MACRO_EXEC DESCENDING_PL2 $TIME=2012/11:02:07:27:47
# Orbit# 184 PERIGEE: Inertial Maneuver Commands
@FCT_SetScState housekeeping $TIME=2012/11:02:13:57:50
@ECT_SetHTRCmd CATBED_5N_HTR,ON $TIME=2012/11:02:14:00:40
@ACT_SetKFInputSelect GND_CMD, 0, 0, 0, 0 $TIME=2012/11:02:14:45:40
@ACT_SetEstUpdateEnables ENABLE, DISABLE $TIME=2012/11:02:14:45:41
@FCT_SetFcMode burn $TIME=2012/11:02:14:52:40
@ACT_SetInrDir -0.786493,-0.561456,-0.257285 $TIME=2012/11:02:14:53:40
@ACT_SetLrTarget ACS_INERTIAL $TIME=2012/11:02:14:54:40
@ACT_SetThrustTime 660 $TIME=2012/11:02:14:55:35
@ACT_SetThrustEnable ENABLE $TIME=2012/11:02:14:55:40
@ACT_SetThrustEnable DISABLE $TIME=2012/11:02:15:05:40
@ECT_SetHTRCmd CATBED_5N_HTR,OFF $TIME=2012/11:02:15:05:41
@ACT_SetThrustTime 0 $TIME=2012/11:02:15:06:10
@ACT_SetStaticZrate ESTIMATOR, 0.418 $TIME=2012/11:02:15:20:50
@ACT_SetKFInputSelect STA_PCT_VALID, 48,18,23,53 $TIME=2012/11:02:15:21:00
@FCT_SetFcMode Mission $TIME=2012/11:02:15:21:40
end
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Orbit# 184
IBEX,AUWA01,DELETE,10/25/12,299,06:00:00,10/25/12,299,06:35:00,,LAHO 40K IBEX Orbit# 183 Tracking Contact(12 Asc)
IBEX,AUWA01,DELETE,10/25/12,299,11:00:00,10/25/12,299,12:00:00,,LAHO 2K IBEX Orbit# 183 LUT Upload Contact/Blind_Acq (16 Asc)
IBEX,USHI01,DELETE,10/26/12,300,01:30:00,10/26/12,300,02:30:00,,LAHO 2K IBEX Orbit# 183 LUT Upload Contact/Blind_acq (26 Asc)
IBEX,USHI01,ADD,10/26/12,300,01:30:00,10/26/12,300,03:00:00,,LAHO 2K IBEX Orbit# 183 LUT Upload Contact/Blind_acq (26 Asc)
IBEX,USHI01,DELETE,10/26/12,300,03:30:00,10/26/12,300,04:30:00,,LAHO 2K IBEX Orbit# 183 LUT Upload Contact/Blind_acq (27 Asc)
IBEX,USHI01,ADD,10/26/12,300,04:00:00,10/26/12,300,05:00:00,,LAHO 2K IBEX Orbit# 183 LUT Upload Contact/Blind_acq (27 Asc)
IBEX,USHI01,ADD,10/30/12,304,08:00:00,10/30/12,304,08:35:00,,LAHO 2K IBEX Orbit# 184 Apogee Contact (46 Desc)
IBEX,USHI01,ADD,11/02/12,307,10:00:00,11/02/12,307,11:00:00,,LAHO 160K IBEX Orbit# 184 SSR_Dump/Tracking Contact (13 Desc)
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